C22F1/183

MANUFACTURING METHOD FOR NICKEL-BASED ALLOY PRODUCT OR TITANIUM-BASED ALLOY PRODUCT

Provided is a method for producing a Ni- or Ti-based alloy product, the method capable of reliably locally cooling and effectively cooling. The method includes the steps: heating and holding a hot working material of a Ni- or Ti-based alloy after hot forging or hot ring rolling at a solution treatment temperature to obtain a material held in a heated state, and cooling the material held in a heated state to obtain a solution-treated material. The cooling step includes carrying out local cooling by contacting a cooling member with a part of a surface of the material held in a heated state.

METHOD FOR PRODUCING NICKEL-BASED ALLOY PRODUCT OR TITANIUM-BASED ALLOY PRODUCT

Provided is a method for producing a Ni- or Ti-based alloy product, the method capable of locally increasing the cooling rate and effectively cooling. The method includes the steps: preliminarily processing a hot working material of a Ni- or Ti-based alloy after hot working into a predetermined shape; heating and holding the material at a solution treatment temperature to obtain a material held in a heated state; and cooling the material held in a heated state to obtain a solution-treated material. The cooling step includes placing a flow path-forming member having a space for forming a flow path for a fluid on a surface of the material held in a heated state to form a fluid flow path defined by the surface of the material held in a heated state and an inner surface of the space of the flow path-forming member; and allowing a fluid to flow in the fluid flow path so that the fluid in the flow path locally cools a part of the surface of the material held in a heated state.

MEDICAL LEADS AND TECHNIQUES FOR MANUFACTURING THE SAME

In some examples, the disclosure relates to a medical device such as an implantable medical lead. The medical lead may include: a lead body including an electrically conductive lead wire; an electrical contact on a proximal portion of the lead body, the electrical contact including a contact substrate; and an electrode on a distal portion of the lead body, the electrode including an electrode substrate, wherein the electrode substrate is electrically coupled to the contact substrate via the electrically conductive lead wire, wherein the lead wire is formed of a composition comprising titanium or titanium alloys, wherein the electrode substrate is formed of a first beta-titanium alloy, and wherein the contact substrate is formed of a second beta-titanium alloy.

MEDICAL TITANIUM ALLOY HAVING HIGH FATIGUE STRENGTH, AND HOT PROCESSING AND HOT TREATMENT METHOD THEREFOR AND DEVICE THEREOF
20220372606 · 2022-11-24 ·

A medical titanium alloy having high fatigue strength, and a hot processing and heat treatment method therefor and the related device thereof. The medical titanium alloy contains 3.0-6.0% of vanadium, 5.0-7.0% of aluminum, and 4.0-8.0% of copper and titanium in balance. By using the above-mentioned configuration, the present invention enables the medical titanium alloy to possess higher fatigue strength.

Titanium cast product for hot rolling unlikely to exhibit surface defects and method of manufacturing the same

Provided is a titanium cast product for hot rolling made of commercially pure titanium, the titanium cast product including a melted and resolidified layer in a range of more than or equal to 1 mm in depth on a surface serving as a rolling surface, the melted and resolidified layer being obtained by adding one or more elements out of any one of or both of at least one α stabilizer element and at least one neutral element to the surface, and melting and resolidifying the surface. An average value of a total concentration of the at least one α stabilizer element and the at least one neutral element in the range of more than or equal to 1 mm in depth is higher than a total concentration of the at least one α stabilizer element and the at least one neutral element in a base metal by, in mass %, more than or equal to 0.1% and less than 2.0%.

Thermally stabilized fastener system and method

A thermally stabilized fastener system and method is disclosed. The disclosed system/method integrates a fastener (FAS) incorporating a faster retention head (FRH), fastener retention body (FRB), and fastener retention tip (FRT) to couple a mechanical member stack (MMS) in a thermally stabilized fashion using a fastener retention receiver (FRR). The MMS includes a temperature compensating member (TCM), a first retention member (FRM), and an optional second retention member (SRM). The TCM is constructed using a tailored thermal expansion coefficient (TTC) that permits the TCM to compensate for the thermal expansion characteristics of the FAS, FRM, and SRM such that the force applied by the FRH and FRR portions of the FAS to the MMS is tailored to a specific temperature force profile (TFP) over changes in MMS/FAS temperature. The TCM may be selected with a TTC to achieve a uniform TFP over changes in MMS/FAS temperature.

THERMALLY STABILIZED FASTENER SYSTEM AND METHOD

A thermally stabilized fastener system and method is disclosed. The disclosed system/method integrates a fastener (FAS) incorporating a faster retention head (FRH), fastener retention body (FRB), and fastener retention tip (FRT) to couple a mechanical member stack (MMS) in a thermally stabilized fashion using a fastener retention receiver (FRR). The MMS includes a temperature compensating member (TCM), a first retention member (FRM), and an optional second retention member (SRM). The TCM is constructed using a tailored thermal expansion coefficient (TTC) that permits the TCM to compensate for the thermal expansion characteristics of the FAS, FRM, and SRM such that the force applied by the FRH and FRR portions of the FAS to the MMS is tailored to a specific temperature force profile (TFP) over changes in MMS/FAS temperature. The TCM may be selected with a TTC to achieve a uniform TFP over changes in MMS/FAS temperature.

TITANIUM ALLOY
20220364206 · 2022-11-17 · ·

To provide a titanium alloy with superior corrosion resistance. The titanium alloy, having α- and β-phases, containing: by mass %, Fe: 0.010 to 0.300%, Ru: 0.010 to 0.150%, Cr: 0 to 0.10%, Ni: 0 to 0.30%, Mo: 0 to 0.10%, Pt: 0 to 0.10%, Pd: 0 to 0.20%, Ir: 0 to 0.10%, Os: 0 to 0.10%, Rh: 0 to 0.10%, one type or two or more types of La, Ce, and Nd: 0 to 0.10% in total, one type or two or more types of Cu, Mn, Sn, and Zr: 0 to 0.20% in total, C: 0.10% or less, N: 0.05% or less, 0: 0.20% or less, H: 0.100% or less, with the balance made up of Ti and impurities, wherein an average A-value in Expression (1), which represents a composition ratio of elements contained in β-phase crystal grains, is in a range of 0.550 to 2.000, is used.

THERMALLY STABILIZED FASTENER SYSTEM AND METHOD

A thermally stabilized fastener system and method is disclosed. The disclosed system/method integrates a fastener (FAS) incorporating a faster retention head (FRH), fastener retention body (FRB), and fastener retention tip (FRT) to couple a mechanical member stack (MMS) in a thermally stabilized fashion using a fastener retention receiver (FRR). The MMS includes a temperature compensating member (TCM), a first retention member (FRM), and an optional second retention member (SRM). The TCM is constructed using a tailored thermal expansion coefficient (TTC) that permits the TCM to compensate for the thermal expansion characteristics of the FAS, FRM, and SRM such that the force applied by the FRH and FRR portions of the FAS to the MMS is tailored to a specific temperature force profile (TFP) over changes in MMS/FAS temperature. The TCM may be selected with a TTC to achieve a uniform TFP over changes in MMS/FAS temperature.

Hydrogenation-dehydrogenation method for TiAl alloy and method for producing TiAl alloy powder

A hydrogenation-dehydrogenation method for a TiAl alloy includes performing hydrogenation treatment of the TiAl alloy in an environment of a set temperature equal to or higher than a temperature at which phase transformation to a β phase starts; and performing dehydrogenation treatment of the TiAl alloy which has been subjected to the hydrogenation treatment. The set temperature ranges from 1,100° C. to 1,600° C.